View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 37223U 10062B 11152.36844328 0.00000635 00000-0 88754-4 0 07
2 37223 71.9713 73.6151 0021634 311.5989 48.3343 14.77415682 02
Epoch (UTC): | 01 June 2011 08:50:33 |
Eccentricity: | 0.0021634 |
inclination: | 71.9713° |
perigee height: | 622 km |
apogee height: | 652 km |
right ascension of ascending node: | 73.6151° |
argument of perigee: | 311.5989° |
revolutions per day: | 14.77415682 |
mean anomaly at epoch: | 48.3343° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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